Optimization of Airfoil Blend Limits With As-Manufactured Geometry Finite Element Models
Author:
Affiliation:
1. Engine Integrity Branch, Turbine Engine Division, Aerospace Systems Directorate, AFRL Wright-Patterson AFB, WPAFB, OH 45433
2. Advanced Engineering Solutions, Lafayette, CO 80026
3. Perceptive Engineering Analytics, Minneapolis, MN 55418
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
https://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/144/3/031013/6818794/gtp_144_03_031013.pdf
Reference33 articles.
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3. Impact of Manufacturing Variability and Nonaxisymmetry on High-Pressure Compressor Stage Performance;ASME J. Eng. Gas Turbines Power,2012
4. Uncertainties of an Automated Optical 3D Geometry Measurement, Modeling, and Analysis Process for Mistuend Integrally Bladed Rotor Reverse Engineering;ASME J. Eng. Gas Turbines Power,2013
5. Automated Finite Element Model Mesh Updating Scheme Applicable to Mistuning Analysis,2014
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